Device and process for acquisition of measurements using a digital communication bus, particularly used during aircraft tests

ABSTRACT

The invention relates to a device for acquisition of measurements using a digital communication bus ( 10 ) and a computer system. The device includes a bus arbitrator, several items of slave equipment, and two line termination devices. The bus arbitrator ( 11 ) is connected to the bus ( 10 ), with the function of acting as the bus master. The bus arbitrator synchronizes measurements made using sensors ( 14 ). The several items of slave equipment ( 13 ) are connected on the bus ( 10 ), to which these sensors ( 14 ) are connected. The first of the two line termination devices is integrated in the bus arbitrator ( 11 ) and the second is integrated into slave equipment ( 13 ) at the other end of the bus ( 10 ) opposite the bus arbitrator ( 11 ).

STATEMENT OF CROSS-RELATED APPLICATIONS

This application is a divisional application based on U.S. applicationSer. No. 10/390,240, entitled “Device and Process For Acciuisition OfMeasurements Using A Digital Communication bus, Particularly Used DuringAircraft Tests” by Laurent Viard, Gilles Freaud and Pierre Perez, whichwas filed on Mar. 14, 2003 now U.S. Pat. No. 6,937,957 which claimspriority based on French Patent Application No. 02 03217, entitled“Device and Process For Acquisition Of Measurements Using A DigitalCommunication bus, Particularly Used During Aircraft Tests” by LaurentViard, Gilles Freaud and Pierre Perez, which was filed on Mar. 15, 2002,and which was not published in English.

TECHNICAL FIELD

This invention relates to a device and process for acquisition ofmeasurements using a digital communication bus, particularly used duringaircraft tests.

STATE OF PRIOR ART

A known method of acquiring measurements consists of using multiplexersreceiving measurement signals from analog and/or digital sensors asinput. These multiplexers digitize signals originating from analogsensors and format signals from digital sensors. Output signals fromthese multiplexers can then be sent to an acquisition computer.

In aeronautics, this type of output signal is frequently made accordingto the ARINC 429 standard. However, connections made using this standardonly enable a limited throughput. Several connections then have to bemade between each multiplexer and the acquisition computer. When thenumber of measurements made per unit time is large, it is frequent touse one link of this type for each multiplexer. The result is a verylarge volume of wiring, with the corresponding disadvantages in terms ofcost, volume, weight, etc.

A person skilled in the art, faced with the need to reduce the wiringvolume, may decide to use a digital communication bus between themultiplexers and the computer for the acquisition of measurements.

This could be a CAN bus (ISO standard 11898:1993 (E)) used in theautomobile field. But there are several disadvantages with this type ofbus that make it unsuitable for the envisaged application of acquiringmeasurements during aircraft tests:

-   -   it is not synchronous and therefore cannot be used to make        measurements using different sensors at the same times,    -   its maximum throughput (1 Mbit/s) is not sufficiently high for        the envisaged application and the maximum length of the        connections is insufficient; the routing of connections in an        aircraft can be as long as or longer than a hundred meters.

This bus could be a FIP bus (NFC46-602, NFC46-603, NFC46-604 standards)or the WorldFIP bus derivative of it (EN50170 standard—volume 3), usedin the industrial logic controllers field. This type of bus has adeterministic nature (possibility of synchronizing measurements fromdifferent sensors), but it requires the use of specific large componentswhich have the following disadvantages:

-   -   these components can cause integration problems in aircraft        equipment,    -   these components are only available in “commercial” temperature        ranges, whereas the position of some multiplexers (for example        close to engine areas) requires the use of components that can        operate at higher temperatures (up to 105° C.),    -   their maximum throughput of 2.5 Mbit/s is not always enough to        transmit all the measurements made.

Furthermore, a FIP bus of this type is intended to be sufficientlyuniversal to federate different types of equipment (logic controllers,speed variators, etc.). The protocol used is thus fairly complex andtherefore requires the exchange of a large volume of information on thebus, which is a problem in itself when the “useful” data volume itselfis high, as is the case for cyclic measurement acquisitions.

The purpose of the invention is to propose a device and a method foracquisition of measurements using a digital communication bus toovercome the disadvantages mentioned above.

PRESENTATION OF THE INVENTION

The purpose of the invention is a device for acquisition of measurementsusing a digital communication bus and a computer system characterized inthat it comprises:

-   -   a bus arbitrator connected to this bus, with the function of        acting as the bus master and which synchronizes measurements        made using sensors,    -   several items of slave equipment connected on this bus, to which        these sensors are connected,    -   two line termination devices; the first being integrated in the        bus arbitrator and the second being integrated into slave        equipment at the end of the bus opposite the bus arbitrator.

The said device may also comprise at least one intelligent sensorcomprising at least one measurement channel connected directly to thebus.

Advantageously, the bus is composed of a cable with two shielded twistedpairs:

-   -   a first pair being used for data exchanges between the bus        arbitrator and slave equipment,    -   a second pair being used for transporting a data validation        clock.

The bus is split into several segments, the ends of which are connectedto the slave equipment connectors, one end of one of the segments beingconnected to the bus arbitrator, the interconnections between thesevarious segments and the connection lines between the slave equipmentand the bus being made within the slave equipment.

A junction element can replace slave equipment, the connection of thiselement being compatible with the connection of the slave equipment toguarantee continuity of the bus and the bus shielding.

Slave equipment may be composed of two types of multiplexers:

-   -   multiplexers of a first type, each of which receives 16 analog        input channels,    -   multiplexers of a second type, each of which receives 32 analog        inputs.

Another purpose of the invention is a process for the acquisition ofmeasurements using a digital communication bus, a computer system, a busarbitrator connected to this bus which acts as bus master and whichsynchronizes measurements made using sensors, and several items of slaveequipment connected to this bus to which these sensors are connected,characterized in that the bus arbitrator uses a cyclic exchange ofvariables to acquire measurements from sensors through the slaveequipment.

Advantageously, the bus arbitrator comprises a scanning table composedof an ordered sequence of identifiers of variables to be queried duringan elementary data scanning cycle. This table is fixed and unchangeable.This table comprises two parts; a first part related to the acquisitionof measurements, a second part related to the acquisition of statusvariables of the different slave equipment.

In another operating mode, the bus arbitrator uses a non-periodicexchange of variables to make data transfers either from the said busarbitrator to the slave equipment, or from slave equipment to the saidbus arbitrator. The bus arbitrator orders circulation of a startdownload/remote read data transfer identification frame to trigger thedata transfer.

When transferring download data only, the slave equipment that receivesthe data begins by acknowledging the received identification frame. Thenext step is an exchange of data sent by the bus arbitrator (download)or by the sending slave equipment (remote read), with an acknowledgementof each exchange by the data receiver.

For a transfer of download data, the bus arbitrator terminates theexchange by sending an end of transaction indication frame that isacknowledged by the slave equipment concerned.

For a transfer of remote read data, the sending slave equipmentindicates the end of the exchange by sending an end of transactionindication frame to the bus arbitrator.

Advantageously, the said measurement acquisition device may be usedduring tests on an aircraft.

The use of a digital communication bus like that described above has theadvantage that no special components are necessary; the physical layeris made by means of “driver” circuits for RS485 type connections; thelink layer and the application layer use programmable components (DSP ormicro controller, FPGA). These various components are available fortemperature ranges compatible with the envisaged application.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 illustrates a measurement acquisition device with an architecturebased on a digital communication bus for application of the processaccording to the invention.

FIG. 2 illustrates the clock and data signals used in the device in FIG.1.

FIG. 3 illustrates an embodiment of the device according to theinvention.

FIG. 4 illustrates the communication protocol used in the deviceaccording to the invention.

FIG. 5 illustrates the CTRL+ID check field for a frame of thecommunication protocol used in the device according to the invention.

FIG. 6 illustrates an example embodiment of the invention.

DETAILED PRESENTATION OF EMBODIMENTS

The following description defines physical layer and data link layerelements for a digital communication bus dedicated to informationexchange between sensors and/or sensor multiplexers and a computeracquisition system, according to the ISO model.

The Open Systems Interconnection Basic Reference Model, simply calledthe ISO model (ISO standard 7498—Part 1) is an abstract reference modelused to create interconnection and cooperation standards betweendistributed systems.

This model defines an architecture consisting of several layersapplicable for all network categories in which:

-   -   the physical layer is used for the transmission of the bits in a        data block. It specifies the mechanical, electrical and        functional rules and procedures related to data circuits (one        data circuit is formed by a communication line and by the means        necessary to transmit information on the line). It provides        means of setting up a physical connection between two items of        equipment, maintaining this connection during exchanges and        releasing it at the end of exchanges.    -   the data link layer was initially introduced to overcome        problems created by data circuits. These data circuits used to        transmit bits are sensitive to noise (attenuation, phase        distortion, parasites, etc.) and have an error rate that is        unacceptable to users who operate the interconnected elements.        The role of the data link layer is to set up logical connections        between entities that would like to exchange data. Logical        connections offered by the data link level are error free. At        this level, data are organized in the form of frames.        Transmission errors and frame loss and duplication problems are        handled by the data link layer.

As illustrated in FIG. 1, the measurement acquisition device accordingto the invention is structured around a digital communication bus 10 onwhich a bus arbitrator 11 is connected to act as the bus master,together with a number of slave equipments 13 to which sensors 14 areconnected; the computer system used is well known to a person skilled inthe art and is not shown.

As shown in this FIG. 1, intelligent sensors 16 may be connecteddirectly onto the digital communication bus 10. These types ofintelligent sensors 16 may comprise one measurement channel (for exampletemperature, pressure, etc.), or several measurement channels integratedin the same sensor; for example a first pressure or relative humiditymeasurement, plus a temperature measurement to correct the said firstmeasurement.

Throughout the remainder of the description, the term “slave equipment13” will be used to denote slave items of equipment 13 themselvestogether with the intelligent sensors 16.

Physical Layer

Physically, this digital communication bus 10 is connected in a knownmanner according to the RS485 standard. It thus comprises linetermination devices 15 composed of impedances with values of 120 ohms.

This bus 10 is composed of a cable with two shielded twisted pairs (2p):

-   -   a first pair used to exchange data between the bus arbitrator 11        and slave equipment 13,    -   a second pair used for transport of a data validation clock.

The shielding in this cable is made continuous throughout its length.Each shielding at each slave equipment 13 is connected to the mechanicalground through a capacitor. The shielding is connected directly to themechanical ground at the bus arbitrator 11.

Pull-up and pull-down resistances at the bus arbitrator 11 are used tofix the voltages on the data and clock lines or pairs for the highimpedance status. The value of these resistances is 390 ohms.

The configuration of the bus 10 is such that there is a single pathbetween all equipment 11 and 13 dialoging on this bus. There must not bea closed loop.

Data transmitted on this bus 10 are encoded in the NRZ (non return tozero) format as shown in FIG. 2A:

-   -   a logical “1” corresponds to a high (H) physical level,    -   a logical “0” corresponds to a low (B) physical level.

As shown in FIG. 2B, the data (DATA) sent on the first cable pair areaccompanied by a clock (CLK) emitted on the second pair. This clock,sent on the second pair, validates the data simultaneously transmittedon the first pair at its rising front.

When no data are being sent on the bus, the two clock and data lines arein the “high impedance” status which corresponds to a logical “1” due tothe presence of the above mentioned pull-up and pull-down resistances.

In the embodiment of the device according to the invention illustratedin FIG. 3, which facilitates the installation (cables, connections) ofthe bus, one of the two line termination devices 15 is integrated intothe bus arbitrator 11, and the other line termination device isintegrated into the slave equipment 13 at the other end of the bus 10.

To achieve this, each item of slave equipment 13 comprises a resistancewith an appropriate value (120 ohms) that can be connected to the bus 10using at least one shunt 17 connected to the connector 18 on the slaveequipment considered.

As illustrated in FIG. 3, the bus 10 is advantageously split intoseveral segments, the ends of which are connected to the connectors 18of the slave equipment 13 or the sensors 16, one end of one of thesegments, for example the first segment, being connected to the busarbitrator 11. Interconnections between these different segments and theconnection lines or stubs between slave equipment 13 and the bus 10, aremade inside slave equipment 13, which minimizes and fixes the length ofthe stubs. The result is that these stubs cannot become sources forreflections of bus signals and therefore sources of disturbances of dataexchanges.

If slave equipment 13 has to be removed from the bus 10, it can bereplaced by a junction element 19 which has connections compatible withit, to achieve continuity between the two pairs of the cable and itsshielding.

Data Link Layer

The device according to the invention described above has two operatingmodes:

-   -   a first operating mode in which the bus arbitrator 11 acquires        measurements originating from sensors 14 through slave equipment        13, through a cyclic exchange of variables,    -   a second operating mode in which the bus arbitrator 11 makes        data transfers either from the said bus arbitrator 11 to the        slave equipment 13 (download), or from slave equipment 13 to the        bus arbitrator 11 (remote read), the transfers made according to        the second mode being non-periodic. For example, data        transmitted during these transfers may relate to settings or        programming of slave equipment 13.

In the first embodiment, the bus arbitrator 11 comprises a scanningtable composed of an ordered sequence of identifiers of variables to bequeried during an elementary data scanning cycle, as shown in table 1 atthe end of the description. This table is fixed and unchangeable,regardless of the slave equipment 13 being present or absent on the bus10.

This table comprises two parts:

-   -   a first part related to acquisition of measurements, for example        in increasing order of the numbers of slave equipment 13 and        variable addresses, produced for a given slave equipment, (for        example measurements 1, measurements 2),    -   a second part related to acquisition of status variables from        the different slave equipment 13, for example in increasing        order of the numbers of slave equipment 13.

The size of this table may initially be fixed arbitrarily.

In the second operating mode, the bus arbitrator 11 causes circulationof a start download/remote read data transfer identification frame toinitiate the data transfer.

In the case of download data transfer only, the slave equipment 13 thatis recognized as the recipient of the data begins by acknowledging thereceived identification frame. A data exchange follows, sent by the busarbitrator 11 (download) or by the sending slave equipment 13 (remoteread), with acknowledgement of each exchange by the data receiver.

In the case of a download data transfer, the bus arbitrator 11terminates the exchange by sending an end of transaction indicationframe acknowledged by the slave equipment concerned.

In the case of a remote read data transfer, the sending slave equipment13 indicates the end of the exchange by returning an end of transactionindication frame to the bus arbitrator 11.

The communication protocol used between the bus arbitrator 11 and theslave equipment 13 is based on an exchange of information frames likethat shown in FIG. 4.

The meaning of the abbreviations shown in this figure are as follows:

FSS: Frame Start Sequence PRE: PREamble FSD: Frame Start Delimiter CAD:Control And Data CTRL + ID: ConTRoL + IDentifier (ID) DATA: Data FCS:Frame Check Sequence FES: Frame End Sequence FED: Frame End DelimiterPST: PoSTamble

Therefore, each frame comprises a frame start identification sequence(FSS), a control field (CTRL+ID) indicating the nature of the frame(cyclic variable read, download, remote read, etc.) and the variableconcerned, a data area (DATA), a transmission error check code (FCS),and a frame end identification sequence (FES).

The error check code (FCS) is calculated by applying a polynomial suchas for example X¹⁶+X¹²+X¹¹+X¹⁰+X⁸+X⁷+X⁶+X³+X²+X+1, (DATA) fields, andthen complementing the 16-bit word thus obtained.

If there is a difference between the error check code FCS received andthe error check code FCS recalculated by the frame recipient, it isconsidered that this frame is lost. Loss of a frame related tocyclically exchanged variables is usually not very serious because thevalue of the variable is distributed again during the next scanningcycle.

As illustrated in FIG. 5A, the CTRL+ID field is composed of two parts:

-   -   a “check” part that indicates the nature of the frame; for a        frame sent by the bus arbitrator, the bits considered specify        the current exchange type; possible values are illustrated in        table 2. For a response frame, these bits indicate the current        exchange type; possible values are illustrated in table 3.    -   an “identifier” part itself subdivided into two fields:        -   subscriber address (or slave equivalent),        -   variable address.

Variable identifiers are illustrated in FIG. 5B. Download/remote readdata identifiers are illustrated in FIG. 5C.

The number of bits indicated in FIGS. 5A, 5B and 5C are applicable forone possible embodiment.

The “identifier” part is used to specify which variable of which slaveequipment 13 is to be read or written. A subscriber address equal tozero can be used to simultaneously address all slave equipment 13. Thisfunction is used particularly to send synchronization pulses to allslave equipment 13 for the acquisition of measurements from sensors atthe same instant on each slave equipment 13 with a small time errormargin.

The length of the data (DATA) field is fixed when the device isdesigned. It may be equal to three values depending on the frame type:

-   -   a first value related to the first operating mode, corresponding        to a query frame for slave equipment 13 by the bus arbitrator 11        depending on the variables scanning table,    -   a second value related to the first operating mode corresponding        to a frame containing variables (measurements and/or status)        returned by slave equipment 13 following a query by the bus        arbitrator 11, and    -   a third value related to the second operating mode,        corresponding to a download/remote read frame.

Example Embodiment of the Invention

In one example embodiment illustrated in FIG. 6, the device according tothe invention comprises not more than 16 (for example 5) slave units 13.The length of the bus 10 is less than or equal to 100 meters. Equipment11 and 13 connected to the bus 10 communicate at a rate of 4.167Mbits/s. The variable scanning frequency is equal to 128 samples persecond.

Slave equipment is composed of two types of multiplexers:

-   -   a first type of multiplexers 13, each of which receives 16        analogue input channels A1n . . . A16, for example strain        gauges, temperature or voltage probes,    -   a second type of multiplexers 13′, each of which receives 32        analogue inputs B1 . . . B32, for example temperature probes.

Before the beginning of a scanning cycle, the bus arbitrator 11 sends asynchronization frame to all slave multiplexers 13 and 13′ so that theycan acquire data at approximately the same moment.

Furthermore, the bus arbitrator 11 sends a frame twice a secondcorresponding to another type of synchronization which has the effect ofinitializing start up of onboard software in this multiplexerimmediately after one of the said multiplexers has started, so that thissoftware is executed approximately synchronously with the execution ofsoftware onboard the computer system controlling the acquisition ofmeasurements through the bus arbitrator and onboard the othermultiplexers connected to the same communication bus.

The use of the said synchronization frames is a means of obtaining amaximum value of the phase shift (time difference between themeasurements from any two sensors) less than 0.1°.

The frame length is fixed when the system is designed. The DATA fieldcontains 0 byte in the case of query frames to slave equipment 13 sentby the bus arbitrator 11, 36 bytes in the case of variable return framessent from slave equipment 13, and 128 bytes in the case ofdownload/remote read frames. If the number of bytes is greater than thevolume of data to be transmitted, unused bytes are fixed at an arbitraryvalue (for example equal to zero).

TABLE 1 Subscriber physical address Variable produced Identificationcode 1 Measurements 1 Code 1 1 Measurements 2 Code 2 2 Measurements 1Code 3 2 Measurements 2 Code 4 3 Measurements 1 Code 5 . . . . . . . . .16 Measurements 1 Code 31 16 Measurements 2 Code 32 1 Status Code 33 2Status Code 34 . . . . . . . . . 16 Status Code 48

TABLE 2 5 4 3 2 1 0 Identification frame 0 0 0 0 0 1 Identified variablemedium allocation 0 0 0 1 0 0 Start transfer of download data 0 0 1 1 00 End transfer of download data 0 0 0 1 1 0 Start transfer of remoteread data 0 1 0 1 1 1 Positive acknowledgement transfer of remote readdata

TABLE 3 5 4 3 2 1 0 Response frame 1 0 0 0 0 1 Identified variableresponse 1 1 0 1 0 0 Positive acknowledgement start of download datatransfer 1 0 0 1 0 0 Negative acknowledgement start of download datatransfer 1 1 0 1 0 1 Positive acknowledgement download data transfer 1 11 1 0 0 Positive acknowledgement end of download data transfer 1 0 1 1 00 Negative acknowledgement end of download data transfer 1 1 0 1 1 1Transfer of remote read data 1 1 1 1 1 1 End transfer of remote readdata

1. A process for the acquisition of measurements using a digitalcommunication bus, a computer system, a bus arbitrator connected to thisbus which acts as bus master and which synchronizes measurements madeusing sensors, and several items of slave equipment connected to thisbus to which these sensors are connected, comprising: obtaining aseciuence of identifiers of variables for a scanning cycle from a fixedand unchangeable scanning table located in the bus arbitrator; scanningmeasurements by the sensors in accordance with the scanning cycle; andacquiring the measurements from the sensors through the slave equipmentin response to the sequence of the identifiers of variables.
 2. Processaccording to claim 1, in which the scanning table comprises an orderedsequence of identifiers of variables to be queried during an elementarydata scanning cycle.
 3. Process according to claim 2, wherein scanningmeasurements further includes detecting analog signals from analog inputchannels of the slave equipments.
 4. Process according to claim 3,wherein the obtaining a sequence of identifiers of variables for ascanning cycle from a fixed and unchangeable scanning table furtherincludes identifying a first part related to the acquisition ofmeasurements and a second part related to the acquisition of statusvariables of the different slave equipment.
 5. Process according toclaim 1, in which the bus arbitrator uses a non-periodic exchange ofvariables to make data transfers either from the bus arbitrator to theslave equipment, or from slave equipment to the bus arbitrator. 6.Process according to claim 5, in which the bus arbitrator orders thecirculation of a start download/remote read data transfer identificationframe to trigger the data transfer.
 7. Process according to claim 6, inwhich, in the case of a transfer of download data only, the slaveequipment that receives the data begins by acknowledging the receivedidentification frame, and is then followed by an exchange of data sentby the bus arbitrator (download) or by the sending slave equipment(remote read), with an acknowledgement of each exchange by the datareceiver.
 8. Process according to claim 7, in which, in the case of atransfer of download data, the bus arbitrator terminates the exchange bysending an end of transaction indication frame that is acknowledged bythe slave equipment concerned.
 9. Process according to claim 6, inwhich, in the case of a transfer of remote read data, the sending slaveequipment indicates the end of the exchange by sending an end oftransaction indication frame to the bus arbitrator.
 10. The processaccording to claim 1 wherein the slave equipment includes at least onemultiplexer.
 11. The process according to claim 10 further comprising:periodically sending a synchronization frame from the bus arbitrator tosynchronize with the computer system, immediately after said at leastone multiplexer has started.
 12. The process according to claim 10further comprising: periodically sending a synchronizing frame from thebus arbitrator to synchronize with other multiplexers from other slaveequipments, immediately after said at least one multiplexer has started.13. The process according to claim 10 further comprising: periodicallysending a synchronization frame from the bus arbitrator to allmultiplexers, before the beginning of the scanning cycle.